CN217842090U - Air compressor of two structural formulas of admitting air - Google Patents
Air compressor of two structural formulas of admitting air Download PDFInfo
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- CN217842090U CN217842090U CN202221650880.3U CN202221650880U CN217842090U CN 217842090 U CN217842090 U CN 217842090U CN 202221650880 U CN202221650880 U CN 202221650880U CN 217842090 U CN217842090 U CN 217842090U
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Abstract
The utility model discloses an air compressor machine of two inlet structure formulas, including bottom plate and riser, the inside groove has been seted up on the top surface of bottom plate, the inside of inside groove is provided with first pivot, the tip of first pivot runs through the inside of bottom plate, the end fixing of first pivot has the crank, the surface of first pivot is provided with the movable block, the avris of movable block and the inner wall of inside groove are laminated each other, the top of bottom plate is provided with the fuselage, the surface of movable block and fuselage all is fixed with the base, be provided with the connecting rod between the base, this air compressor machine of two inlet structure formulas, through the mutually supporting of parts such as bottom plate, inside groove, first pivot, crank, movable block, fuselage, base and connecting rod for can drive the movable block displacement when first pivot is rotatory, thereby under the effect of connecting rod, the control fuselage goes up and down, has solved current equipment and can's problem of carrying out corresponding regulation according to staff's height.
Description
Technical Field
The utility model relates to an air compressor machine technical field especially relates to an air compressor machine of two structural formulas of admitting air.
Background
The air compressor machine is called air compressor entirely, as the name suggests, is a compressed gas's equipment, and the gas through the compression contains huge kinetic energy, consequently can reach effect such as smashing, for obtaining bigger kinetic energy, some producers can increase the air inlet of air compressor machine, consequently, the air compressor machine of two inlet structure formulas has also produced thereupon.
In the chinese patent with the granted publication number CN213928748U, a pendulum air compressor with a double air inlet structure is disclosed, a motor 13 is installed inside a casing 7 of the device, the control is performed through a control panel 2, a power output end of the motor 13 is connected with a power input end of a transmission shaft 14, the transmission shaft 14 drives a fan blade 15 to rotate, and the surface of the air compressor body 1 is blown to dissipate heat.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing an air compressor machine of two structural formulas of admitting air has height-adjustable festival and low in manufacturing cost's advantage.
The utility model discloses a can realize through following technical scheme:
the utility model provides an air compressor of two air inlet structure formulas, includes bottom plate and riser, the inside groove has been seted up on the top surface of bottom plate, the inside of inside groove is provided with first pivot, the tip of first pivot runs through the inside of bottom plate, the end fixing of first pivot has the crank, the surface of first pivot is provided with the movable block, the avris of movable block and the inner wall of inside groove are laminated each other, the top of bottom plate is provided with the fuselage, the surface of movable block and fuselage all is fixed with the base, be provided with the connecting rod between the base, the inner wall of fuselage is fixed with two the riser, the side of riser is provided with the second pivot, the surface fixing of second pivot has the flabellum, the surface fixing of second pivot has first conical gear, the side of first conical gear is connected with second conical gear, the bottom center department of second conical gear is fixed with the third pivot, the tip of third pivot runs through the inside of fuselage, the tip fixing of third pivot has the transfer gear, be provided with the belt between the transfer gear, the bottom of bottom plate is fixed with the installation shell, the damping spring's inside is fixed with the damping spring, the tip is installed the universal wheel, the power unit is connected with the power unit.
Further setting as follows: the surface of first pivot is provided with two sections opposite screw threads, first pivot and movable block are threaded connection, the movable block is provided with two.
Further setting the following steps: the base is connected with the connecting rod for rotating, and the base and the connecting rod are symmetrically distributed about the longitudinal central axis of the bottom plate.
Further setting the following steps: the first bevel gear and the second bevel gear are in meshed connection, and the first bevel gear and the second bevel gear are symmetrically distributed around the longitudinal central axis of the machine body.
Further setting the following steps: the universal wheel passes through damping spring and constitutes shock-absorbing structure with the installation shell, damping spring and universal wheel all are around the longitudinal center axis symmetric distribution of bottom plate.
Further setting the following steps: the power mechanism comprises a support and a motor, the support is fixed on the outer wall of the machine body, the motor is fixed at the end of the support, and the motor is fixedly connected with one third rotating shaft.
To sum up, the utility model discloses a beneficial technological effect does:
(1) Through mutually supporting of parts such as bottom plate, inside groove, first pivot, crank, movable block, fuselage, base and connecting rod for can drive the movable block displacement when first pivot is rotatory, thereby under the effect of connecting rod, control fuselage goes up and down, has solved the problem that current equipment can't carry out corresponding regulation according to the staff height.
(2) Through mutually supporting of parts such as riser, second pivot, flabellum, first conical gear, second conical gear, third pivot, transfer gear and belt for can drive two sets of flabellums simultaneous operation when the motor moves, thereby solved current equipment and needed a plurality of motor drive, lead to manufacturing cost increase's problem.
Drawings
FIG. 1 is a schematic view of the front cut structure of the present invention;
FIG. 2 is a schematic view of a side-cut installation structure of the movable block of the present invention;
FIG. 3 is a schematic view of the connecting rod installation structure of the present invention;
fig. 4 is a schematic structural view of the power mechanism of the present invention.
Reference numerals: 1. a base plate; 2. an inner tank; 3. a first rotating shaft; 4. a crank; 5. a movable block; 6. a body; 7. a base; 8. a connecting rod; 9. a vertical plate; 10. a second rotating shaft; 11. a fan blade; 12. a first bevel gear; 13. a second bevel gear; 14. a third rotating shaft; 15. a transfer wheel; 16. a belt; 17. mounting a shell; 18. a damping spring; 19. a universal wheel; 20. a power mechanism; 2001. a support; 2002. an electric motor.
Detailed Description
The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention.
Referring to fig. 1-4, for the utility model discloses an air compressor of two inlet structure formulas, including bottom plate 1 and riser 9, inside groove 2 has been seted up to the top surface of bottom plate 1, the inside of inside groove 2 is provided with first pivot 3, the tip of first pivot 3 runs through the inside of bottom plate 1, the end fixing of first pivot 3 has crank 4, the surface of first pivot 3 is provided with movable block 5, the avris of movable block 5 and the inner wall of inside groove 2 are laminated each other, the top of bottom plate 1 is provided with fuselage 6, the surface of movable block 5 and fuselage 6 all is fixed with base 7, be provided with connecting rod 8 between the base 7, the inner wall of fuselage 6 is fixed with two risers 9, the side of riser 9 is provided with second pivot 10, the surface fixing of second pivot 10 has flabellum 11, the surface fixing of second pivot 10 has first bevel gear 12, the side of first bevel gear 12 is connected with second bevel gear 13, the bottom center department of fuselage 13 is fixed with third pivot 14, the tip of third pivot 14 runs through the inside of 6, the end fixing of third pivot 14 has first bevel gear 12, the end fixing has transmission wheel 15, the bottom mounting spring 18 that the universal spring 18 is connected with the bottom mounting shell 17, the universal mounting spring 18 has fixed mounting shell 17, the bottom mounting shell 17 has been installed between the fuselage 18 and the universal mounting shell 17.
The surface of first pivot 3 is provided with two sections opposite screw threads, and first pivot 3 is threaded connection with movable block 5, and movable block 5 is provided with two, and threaded connection can drive movable block 5 displacement when making first pivot 3 rotatory to promote connecting rod 8 and drive fuselage 6 and go up and down, realize altitude mixture control's purpose.
The first bevel gear 12 and the second bevel gear 13 are in meshed connection, the first bevel gear 12 and the second bevel gear 13 are symmetrically distributed about the longitudinal central axis of the machine body 6, and the meshed connection can drive the second rotating shaft 10 to synchronously rotate when the third rotating shaft 14 rotates, so that a power source is provided for the operation of the fan blades 11.
The universal wheel 19 forms a damping structure through the damping spring 18 and the mounting shell 17, the damping spring 18 and the universal wheel 19 are symmetrically distributed about the longitudinal central axis of the bottom plate 1, and the damping mechanism can reduce the bumping amplitude generated when equipment is transferred, so that parts inside the machine body 6 are protected, and the phenomenon of bumping damage is avoided.
The power mechanism 20 comprises a bracket 2001 and a motor 2002, the bracket 2001 is fixed on the outer wall of the body 6, the motor 2002 is fixed on the end portion of the bracket 2001, the motor 2002 is fixedly connected with a third rotating shaft 14, and when the mechanism operates, the third rotating shaft 14 is driven to rotate, so that power output is provided for the subsequent movement of the fan blade 11.
The utility model discloses a theory of operation and beneficial effect do: when the air compressor with the double air inlet structure is used, firstly, the universal wheel 19 is utilized to push equipment to a specified position and the equipment is fixed by utilizing the brake plate, jolting can be generated in the pushing process, but the jolting amplitude can be reduced due to the existence of the damping spring 18, so that the parts inside the machine body 6 are protected, then, a worker can correspondingly adjust the height of the machine body 6 according to the self requirement, if the jolting is required to be increased, the worker can drive the first rotating shaft 3 to rotate through the crank 4, when the first rotating shaft 3 rotates, the threads on the surface can drive the movable blocks 5 to be mutually closed, then, the machine body 6 can be jacked and lifted up by the base 7 and the connecting rod 8 in the closing process of the movable blocks 5 until the requirement is met, the crank 4 stops rotating, otherwise, when the height is required to be reduced, the crank 4 can be reversely rotated, the machine can normally work, when the user starts the motor 2002, the motor can drive the third rotating shaft 14 to rotate, when the third rotating shaft 14 is operated, the third rotating shaft 14 can drive the second rotating shaft 14 to rotate through the second bevel gear 14, and the third rotating shaft 14 can be synchronously rotated through the second bevel gear 14, and the rotating shaft 12, so that the third rotating shaft 14 can rotate when the rotating shaft 14 rotates.
The above, only do the preferred embodiment of the present invention, not limit the protection scope of the present invention according to this, so: all equivalent changes made according to the structure, shape and principle of the utility model are covered within the protection scope of the utility model.
Claims (6)
1. The utility model provides an air compressor machine of two structural formulas of admitting air which characterized in that: comprises a bottom plate (1) and vertical plates (9), wherein an inner groove (2) is formed in the top surface of the bottom plate (1), a first rotating shaft (3) is arranged in the inner groove (2), the end part of the first rotating shaft (3) penetrates through the inner part of the bottom plate (1), a crank (4) is fixed at the end part of the first rotating shaft (3), movable blocks (5) are arranged on the surface of the first rotating shaft (3), the lateral sides of the movable blocks (5) are mutually attached to the inner wall of the inner groove (2), a machine body (6) is arranged above the bottom plate (1), bases (7) are fixed on the surfaces of the movable blocks (5) and the machine body (6), connecting rods (8) are arranged between the bases (7), two vertical plates (9) are fixed on the inner wall of the machine body (6), a second rotating shaft (10) is arranged on the side surfaces of the vertical plates (9), fan blades (11) are fixed on the surface of the second rotating shaft (10), a first bevel gear (12) is fixed on the surface of the second rotating shaft (10), a second bevel gear (13) is connected with the side surface of the first bevel gear (12), a second bevel gear (13) penetrates through the end part of a third bevel gear (14) and a third bevel gear (14) is fixed at the bottom of the center of the rotating shaft (6), the end fixing of third pivot (14) has transfer gear (15), be provided with belt (16) between transfer gear (15), the bottom of bottom plate (1) is fixed with installation shell (17), the inside of installation shell (17) is fixed with damping spring (18), universal wheel (19) are installed to the tip of damping spring (18), power unit (20) are installed to the outer wall of fuselage (6), power unit (20) and one third pivot (14) fixed connection.
2. The air compressor of double air inlet structure formula of claim 1, characterized in that: the surface of the first rotating shaft (3) is provided with two sections of opposite threads, the first rotating shaft (3) is in threaded connection with the movable block (5), and the number of the movable block (5) is two.
3. The air compressor of double air inlet structure formula of claim 1, characterized in that: the base (7) is rotationally connected with the connecting rod (8), and the base (7) and the connecting rod (8) are symmetrically distributed about the longitudinal central axis of the bottom plate (1).
4. The air compressor of double air inlet structure formula of claim 1, characterized in that: the first bevel gear (12) and the second bevel gear (13) are in meshed connection, and the first bevel gear (12) and the second bevel gear (13) are symmetrically distributed around the longitudinal central axis of the machine body (6).
5. The air compressor of double air inlet structure formula of claim 1, characterized in that: the universal wheel (19) and the mounting shell (17) form a damping structure through a damping spring (18), and the mounting shell (17), the damping spring (18) and the universal wheel (19) are symmetrically distributed around the longitudinal central axis of the bottom plate (1).
6. The air compressor of double air inlet structure formula of claim 1, characterized in that: the power mechanism (20) comprises a support (2001) and a motor (2002), the support (2001) is fixed on the outer wall of the machine body (6), the motor (2002) is fixed on the end portion of the support (2001), and the motor (2002) is fixedly connected with one third rotating shaft (14).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202221650880.3U CN217842090U (en) | 2022-06-29 | 2022-06-29 | Air compressor of two structural formulas of admitting air |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202221650880.3U CN217842090U (en) | 2022-06-29 | 2022-06-29 | Air compressor of two structural formulas of admitting air |
Publications (1)
Publication Number | Publication Date |
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CN217842090U true CN217842090U (en) | 2022-11-18 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN202221650880.3U Active CN217842090U (en) | 2022-06-29 | 2022-06-29 | Air compressor of two structural formulas of admitting air |
Country Status (1)
Country | Link |
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CN (1) | CN217842090U (en) |
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2022
- 2022-06-29 CN CN202221650880.3U patent/CN217842090U/en active Active
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